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AMTAS is a consortium of academic institutions, aerospace companies, and government agencies. AMTAS seeks solutions to problems associated with existing, near- and long-term applications of composites and advanced materials for large transport commercial aircraft.

Effects of Finite Element Damage Modeling Parameters in Carbon Fiber Panels Under Mode III Loading

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Effects of Layup and Matrix Toughness on Modeling Notched Carbon Fiber Panels in Out-of-Plane Bending
Mesh Selection for Progressive Failure Modeling of Carbon Fiber Panels in Mode III Shear using an Explicit Finite Element Solver
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